System for performing static and fatigue tests in air ducts that are utilized in aeronautical industry, has programmable control element that controls power station, thermal insulation chamber, pneumatic system, buffer and heating unit

The system has a climate power station that maintains predetermined temperature at an inner side of a thermal insulation chamber. An internal part of the chamber is connected to air ducts. A pneumatic system is provided at an inner side of the air ducts for supplying predetermined pressure to the air ducts. A buffer is provided with a heating unit that warms air before entering the air ducts. A programmable control element controls the power station, the chamber, the pneumatic system, the buffer and the heating unit. The system has a climate power station that maintains predetermined temperature at an inner side of a thermal insulation chamber. An internal part of the chamber is connected to air ducts. A pneumatic system is provided at an inner side of the air ducts for supplying predetermined pressure to the air ducts. A buffer is provided with a heating unit that warms air before entering the air ducts. A programmable control element controls the power station, the chamber, the pneumatic system, the buffer and the heating unit. Sistema para ensayos de fatiga y estáticos en conductos de aire, que dispone de una central climática que mantiene una temperatura predeterminada en el interior de una cámara termo aislante en cuyo interior se aloja el conducto de aire a ensayar al que se le han cerrado sus bocas; un sistema neumático que consta de medios para suministrar al interior del conducto de aire una presión predeterminada para reproducir el ciclo de presión-vacío del ensayo deseado y con un depósito intermedio que consta de medios calefactores que calientan dicho aire antes de introducirse en el conducto de aire del ensayo, con al menos un elemento de control programable para el control de parte o la totalidad del sistema. De aplicación en la industria aeronáutica.